View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 66449U 26145.49040634 +.00000000 +00000-0 +77466-3 0 00003
2 66449 42.9994 200.8983 0002227 266.4515 93.6082 15.27597070 01
| Epoch (UTC): | 25 May 2026 11:46:11 |
| Eccentricity: | 0.0002227 |
| inclination: | 42.9994° |
| perigee height: | 481 km |
| apogee height: | 485 km |
| right ascension of ascending node: | 200.8983° |
| argument of perigee: | 266.4515° |
| revolutions per day: | 15.27597070 |
| mean anomaly at epoch: | 93.6082° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|